The equivalent strain energy method was used to predict the fatigue crack formation life of notched bend specimens with varying notch acuities in two radically different naval alloys: a quenched and tempered steel (Q1N) and an aluminium silicon bronze (ASB). A comparison was made between predicted and experimental crack formation lives, based on a DC electrical potential drop indication of a through crack of 0.05/0.06 mm. For the Q1N steel, where the microstructural features are submicron in size, predicted crack formation lives were in good agreement with experimental results. However, for the ASB alloy with a grain size of 27 μm, very conservative lives were predicted. This difference is attributed to multi-nucleation in the ASB alloy which delayed the formation of a dominant crack to beyond the length defined as crack formation.
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